View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 40071U 26046.18813873 +.00000000 +00000-0 +21316-3 0 00008
2 40071 98.3716 0.6382 0006386 319.8522 40.2221 14.89507820 05
| Epoch (UTC): | 15 February 2026 04:30:55 |
| Eccentricity: | 0.0006386 |
| inclination: | 98.3716° |
| perigee height: | 595 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 0.6382° |
| argument of perigee: | 319.8522° |
| revolutions per day: | 14.89507820 |
| mean anomaly at epoch: | 40.2221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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